The article introduces a methodology for enhancing the performance of an already existing aircraft bracket through the application of topology optimization techniques. The process of topology optimization is conducted utilizing the Siemens NX software. The existing structure is used to generate a preliminary topology, which is then evaluated from low to high stress regions. Then, a new construction with a 50% weight reduction objective was proposed. The topology method is then reapplied to this new structure, evaluating the weak points and failures based on the stress value. The model was then revised to increase its durability and compared to the original model in order to illustrate the optimal weight, volume. The optimal structure was compared with the original model. Eventually, a finished model is manufactured using 3D printing technology. The proposed structure is highly economical, optimized in terms of materials and time, and still ensures the working performance.


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    Titel :

    Topology Optimization Design of an Aircraft Bracket


    Weitere Titelangaben:

    Lect.Notes Mechanical Engineering


    Beteiligte:
    Mo, John P. T. (Herausgeber:in) / Tung, Tran Thanh (Autor:in) / Hiep, Vu Duc (Autor:in) / Quynh, Nguyen Xuan (Autor:in)

    Kongress:

    International Conference on Mechanical, Automotive and Materials Engineering ; 2023 ; Da Nang, Vietnam December 20, 2023 - December 22, 2023



    Erscheinungsdatum :

    25.09.2024


    Format / Umfang :

    9 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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